cutting elements include a substrate, a thermally stable polycrystalline table comprising a superhard material secured to the substrate, and a layer of metal interposed between, and attaching the substrate and the thermally stable polycrystalline table. Methods of forming a cutting element include providing a thermally stable polycrystalline table in a mold, providing a layer of metal on the thermally stable polycrystalline table, distributing a mixture of particles comprising a plurality of hard particles and a plurality of particles comprising a matrix material on the layer of metal, and heating the mold while applying pressure to the mixture of particles to cause the mixture of particles to coalesce and form a substrate and at least partially melt the layer of metal to flow and wet the thermally stable polycrystalline table and the substrate to form an attachment therebetween.
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1. A cutting element, comprising:
a substrate;
a thermally stable polycrystalline table comprising interbonded grains of a superhard material and interstitial spaces among the interbonded grains of the superhard material, the thermally stable polycrystalline table being at least substantially devoid of catalyst material used to form intergranular bonds among the interbonded grains of the superhard material;
a substrate portion interposed between the thermally stable polycrystalline table and the substrate; and
a metal material attaching the substrate to the substrate portion, the metal material extending from proximate the substrate, through the substrate portion, and partially into the thermally stable polycrystalline table, the metal material exhibiting a melting temperature of less than 1320° C.
6. An earth-boring tool, comprising:
a body; and
at least one cutting element attached to the body, the at least one cutting element comprising:
a substrate;
a thermally stable polycrystalline table comprising interbonded grains of a superhard material and interstitial spaces among the interbonded grains of the superhard material, the thermally stable polycrystalline table being at least substantially devoid of catalyst material used to form intergranular bonds among the interbonded grains of the superhard material;
a substrate portion interposed between the thermally stable polycrystalline table and the substrate; and
a metal material attaching the substrate to the substrate portion, the metal material extending from proximate the substrate, through the substrate portion, and partially into the thermally stable polycrystalline table, the metal material exhibiting a melting temperature of less than 1320° C.,
wherein a cutting face of the thermally stable polycrystalline table is located opposite the substrate and is at least substantially free of the metal material.
2. The cutting element of
3. The cutting element of
4. The cutting element of
5. The cutting element of
7. The earth-boring tool of
8. The earth-boring tool of
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This application claims the benefit of the filing date of U.S. Provisional Application Ser. No. 61/388,981, filed Oct. 1, 2010, for CUTTING ELEMENTS, EARTH-BORING TOOLS INCORPORATING SUCH CUTTING ELEMENTS, AND METHODS OF FORMING SUCH CUTTING ELEMENTS, the disclosure of which is hereby incorporated herein in its entirety by this reference.
Embodiments of the present disclosure relate generally to cutting elements that include a table of thermally stable superabrasive material (e.g., thermally stable polycrystalline diamond) attached to a substrate, to earth-boring tools including such cutting elements, and to methods of forming such cutting elements.
Earth-boring tools for forming wellbores in subterranean earth formations may include a plurality of cutting elements secured to a body. For example, fixed-cutter earth-boring rotary drill bits (also referred to as “drag bits”) include a plurality of cutting elements that are fixedly attached to a bit body of the drill bit. Similarly, roller cone earth-boring rotary drill bits may include cones that are mounted on bearing pins extending from legs of a bit body such that each cone is capable of rotating about the bearing pin on which it is mounted. A plurality of cutting elements, typically referred to as “inserts,” may be mounted to each cone of the drill bit.
The cutting elements used in such earth-boring tools often include polycrystalline diamond compact (often referred to as “PDC”) cutting elements, also teamed “cutters,” which are cutting elements that include a polycrystalline diamond (“PCD”) material, which may be characterized as a superabrasive material. Such polycrystalline diamond materials are formed by sintering and bonding together relatively small diamond (synthetic, natural or a combination) grains or crystals, teamed “grit,” under conditions of high temperature and high pressure in the presence of a catalyst (such as, for example, cobalt, iron, nickel, or alloys and mixtures thereof) to form a layer of polycrystalline diamond material, also called a diamond table. These processes are often referred to as high-temperature/high-pressure (or “HTHP”) processes. The cutting element substrate may comprise a cermet material (i.e., a ceramic-metal composite material) such as, for example, cobalt-cemented tungsten carbide. In some instances, the polycrystalline diamond table may be fowled on the cutting element, for example, during the HTHP sintering process. In such instances, cobalt (or other catalyst material) in the cutting element substrate may be swept into the diamond grains or crystals during sintering and serve as a catalyst material for forming a diamond table from the diamond grains or crystals. Powdered catalyst material may also be mixed with the diamond grains or crystals prior to sintering the grains or crystals together in an HTHP process. In other methods, however, the polycrystalline diamond table may be formed separately from the cutting element substrate and subsequently attached thereto.
Upon formation of a diamond table using an HTHP process, catalyst material may remain in interstitial spaces between the grains or crystals of diamond in the resulting polycrystalline diamond table. The presence of the catalyst material in the diamond table may contribute to thermal damage in the diamond table when the cutting element is heated during use due to friction at the contact point between the cutting element and the formation. Polycrystalline diamond cutting elements in which the catalyst material remains in the diamond table are generally thermally stable up to a temperature of about seven hundred fifty degrees Celsius (750° C.), although internal stress within the polycrystalline diamond table may begin to develop at temperatures exceeding about three hundred fifty degrees Celsius (350° C.). This internal stress is at least partially due to differences in the rates of thermal expansion between the diamond table and the cutting element substrate to which it is bonded. This differential in thermal expansion rates may result in relatively large compressive and tensile stresses at the interface between the diamond table and the substrate, and may cause the diamond table to delaminate from the substrate. At temperatures of about seven hundred fifty degrees Celsius (750° C.) and above, stresses within the diamond table may increase significantly due to differences in the coefficients of thermal expansion of the diamond material and the catalyst material within the diamond table itself. For example, cobalt thermally expands significantly faster than diamond, which may cause cracks to form and propagate within the diamond table, eventually leading to deterioration of the diamond table and ineffectiveness of the cutting element.
Furthermore, at temperatures at or above about seven hundred fifty degrees Celsius (750° C.), some of the diamond crystals within the diamond table may react with the catalyst material causing the diamond crystals to undergo a chemical breakdown or conversion to another allotrope of carbon. For example, the diamond crystals may graphitize at the diamond crystal boundaries, which may substantially weaken the diamond table. Also, at extremely high temperatures, in addition to graphite, some of the diamond crystals may be converted to carbon monoxide and carbon dioxide.
To reduce the problems associated with different rates of thermal expansion in polycrystalline diamond cutting elements so-called “thermally stable” polycrystalline diamond (TSD) tables have been developed. A thermally stable polycrystalline diamond table may be formed by leaching the catalyst material (e.g., cobalt) out from interstitial spaces between the diamond grains in the diamond table using, for example, an acid or combination of acids (e.g., aqua regia). Nearly or substantially all of the catalyst material may be removed from the diamond table, or only a portion may be removed. Thermally stable polycrystalline diamond tables in which substantially all catalyst material has been leached from the diamond table have been reported to be thermally stable up to temperatures of about one thousand two hundred degrees Celsius (1,200° C.). It has also been reported, however, that such fully leached diamond tables are relatively more brittle and vulnerable to shear, compressive, and tensile stresses than are non-leached diamond tables. In addition, it is difficult to secure a completely leached diamond table to a supporting substrate. In an effort to provide cutting elements having diamond tables that are more thermally stable relative to non-leached diamond tables, but that are also relatively less brittle and less vulnerable to shear, compressive, and tensile stresses relative to fully leached diamond tables, cutting elements have been provided that include a diamond table in which only a portion of the catalyst material has been leached from the diamond table. For example, it is known to leach catalyst material from the cutting face, from the side of the diamond table, or both, to a desired depth within the diamond table, but without leaching all of the catalyst material out from the diamond table.
In some embodiments, the present disclosure includes cutting elements comprising a substrate, a thermally stable polycrystalline superabrasive table secured on an end of the substrate, and a layer of metal interposed between the substrate and the thermally stable polycrystalline superabrasive table and attaching the substrate to the thermally stable polycrystalline superabrasive table.
In additional embodiments, the present disclosure includes earth-boring tools comprising a body and at least one cutting element attached to the body. The cutting element comprises a substrate, a thermally stable polycrystalline superabrasive table attached to an end of the substrate, and a layer of metal interposed between the substrate and the thermally stable polycrystalline superabrasive table at an end of the thermally stable polycrystalline superabrasive table. At least some of the layer of metal is disposed in at least some interstitial spaces between grains of superabrasive material of the thermally stable polycrystalline superabrasive table. A surface of the thermally stable polycrystalline superabrasive table comprises a cutting face opposite the substrate and is at least substantially free of the metal.
Further embodiments of the present disclosure include methods of forming a cutting element comprising providing a preformed, thermally stable polycrystalline superabrasive table in a mold, providing a layer of metal on the thermally stable polycrystalline superabrasive table in the mold, distributing a mixture of particles comprising a plurality of hard particles and a plurality of particles comprising a matrix material on the layer of metal in the mold, and heating the mold while pressure is applied to the mixture of particles to cause the mixture to coalesce and form a substrate and at least partially melt the layer of metal to flow and wet the thermally stable polycrystalline superabrasive table and the substrate and form an attachment therebetween.
While the specification concludes with claims particularly pointing out and distinctly claiming that which is regarded as embodiments of the present disclosure, various features and advantages of disclosed embodiments may be more readily ascertained from the following description when read in conjunction with the accompanying drawings, in which:
The illustrations presented herein are not meant to be actual views of any particular material or device, but are merely idealized representations that are employed to describe the embodiments of the present disclosure. Thus, the drawings are not necessarily to scale and relative dimensions may have been exaggerated for the sake of clarity. Additionally, elements common between figures may retain the same or similar numerical designation.
Although some embodiments of the present disclosure are depicted as being used and employed in fixed-cutter earth-boring rotary drill bits, persons of ordinary skill in the art will understand that the present disclosure may be employed in any earth-boring tool employing a structure comprising a polycrystalline superabrasive material joined to a supporting substrate. Accordingly, the terms “earth-boring tool” and “earth-boring drill bit,” as used herein, mean and include any type of bit or tool used for drilling during the formation or enlargement of a wellbore in a subterranean formation and include, for example, rotary drill bits, percussion bits, core bits, eccentric bits, bicenter bits, reamers, mills, drag bits, roller cone bits, hybrid bits, and other drilling bits and tools known in the art.
As used herein, the term “polycrystalline superabrasive table” means and includes any structure comprising a plurality of grains (i.e., crystals) of superabrasive material that are bonded directly together by inter-granular bonds. The crystal structures of the individual grains of the material may be randomly oriented in space within the polycrystalline superabrasive material.
As used herein, the term “inter-granular bond” means and includes any direct atomic bond (e.g., covalent, metallic, etc.) between atoms in adjacent grains of superabrasive material.
As used herein, the term “thermally stable polycrystalline superabrasive table” means and includes polycrystalline superabrasive structures as described herein that have been subjected to a process to at least substantially remove catalyst material disposed in the interstitial spaces between grains in at least a portion of the structure. In one embodiment, the thermally stable polycrystalline superabrasive material comprises a polycrystalline diamond compact from which catalyst has been leached from at least a portion thereof.
As used herein, the term “catalyst material” refers to any material that is capable of at least substantially catalyzing the formation of inter-granular bonds between grains of superabrasive, diamond material during an HTHP process. For example, catalyst materials for diamond include cobalt, iron, nickel, other elements from Group VIIIA of the Periodic Table of the Elements, and alloys thereof.
As used herein, the term “superhard material” means and includes any material having a Knoop hardness value of about 3,000 Kgf/mm2 (29,420 MPa) or more. Superhard materials include, for example, diamond and cubic boron nitride. Superhard materials may also be characterized as “superabrasive” materials.
Referring to
Referring to
The substrate 20 may comprise a plurality of hard particles and a plurality of particles comprising a matrix material. For example, the substrate 20 may comprise cemented tungsten carbide or another suitable substrate material, as known in the art. In some embodiments, the thermally stable polycrystalline superabrasive table 18 comprises polycrystalline diamond. In some embodiments, the thermally stable polycrystalline superabrasive table 18 is fully treated such that all or at least substantially all of the catalyst material is removed from interstitial spaces between grains of the polycrystalline superabrasive material exhibiting inter-granular bonding. When it is said that at least substantially all the catalyst material is removed, it is meant that some quantities of catalyst material may remain in isolated pockets that are not interconnected to the otherwise continuous interstitial matrix among the interbonded grains of superhard material of the polycrystalline table 18. In other words, the end of the polycrystalline superabrasive table 18 that is to be attached to the substrate 20 and the opposing end of the polycrystalline superabrasive table 18 that is configured to contact and cut away the underlying earth formation, and all of the volume of polycrystalline superabrasive table 18 therebetween may comprise a polycrystalline superabrasive material having voids or pores filled with air in the interstitial spaces between inter-bonded grains. Furthermore, the polycrystalline superabrasive table 18 may be layered with a differing grain size proximate the end of the polycrystalline superabrasive table 18 to be attached to the substrate 20, or the grain size distribution at least in the area of the polycrystalline superabrasive table 18 proximate that end may be controlled to provide an optimum pore structure that facilitates attachment of the thermally stable polycrystalline superabrasive table 18 to the substrate 20. Although the polycrystalline superabrasive table 18 and the substrate 20 are depicted in
The layer of metal 22 may comprise a metal foil, such as a braze foil. As shown in
Referring to
The preformed substrate component may include a surface coating to enhance bonding between the mixture of particles and the preformed substrate component. For example, a surface coating on a portion or portions of the preformed component intended to bond with the mixture of particles may comprise, molybdenum, tungsten, cobalt, nickel, or an alloy comprising any of these. Further, a surface coating on the exterior of the preformed component may be selected to reduce sliding friction from contact with a formation being drilled, to enhance erosion or abrasion resistance, or a combination of such characteristics. For example, a surface coating to reduce erosion or corrosion may comprise an alloy of chromium. Such exterior surface coatings may also be applied after manufacture of a cutting element 12.
The thermally stable polycrystalline table 18, the layer of metal 22, and the mixture of particles may be subjected to a hot pressing process in some embodiments. For example, a plunger 26 may exert a force F in a direction indicated by an arrow in
The at least partially melted layer of metal 22 may then flow and wet the thermally stable polycrystalline table 18 and the substrate 20. For example, the at least partially melted layer of metal 22 may at least partially infiltrate the thermally stable polycrystalline table 18 in interstitial spaces between grains thereof. The extent to which the at least partially melted layer of metal 22 infiltrates the thermally stable polycrystalline table 18 may be controlled by selecting the material composition of the metal 22, the volume of metal 22 present, the duration of exposure to high heat, the temperature, or any combination of these. For example, the at least partially melted layer of metal 22 may infiltrate between about 10 μm and about 1,000 μm into the thermally stable polycrystalline table 18. More specifically, the at least partially melted layer of metal 22 may infiltrate between about 50 μm and about 200 μm into the thermally stable polycrystalline table 18. In this way, a portion of the thermally stable polycrystalline table 18 (e.g., an end of the thermally stable polycrystalline table 18 opposing the layer of metal 22) may remain at least substantially free of other material (e.g., catalyst material or material of the layer of metal 22) disposed in the interstitial spaces between grains of the material of the thermally stable polycrystalline table 18 during and after attachment of the thermally stable polycrystalline table 18 to the substrate 20. In such embodiments, additional subsequent leaching of the thermally stable polycrystalline table 18 may be unnecessary. However, additional subsequent leaching of the thermally stable polycrystalline table 18 may take place in these or other embodiments. For example, subsequent leaching of the thermally stable polycrystalline table 18 may take place where the at least partially melted layer of non-catalytic metal 22 infiltrates an entire thickness of the polycrystalline table 18.
Additionally or in the alternative, a non-catalyst material may be infiltrated into interstitial spaces between grains of the thermally stable polycrystalline table 18 during the high-temperature/high-pressure process or prior to the high-temperature/high-pressure process from the end of the polycrystalline superabrasive table 18 opposite the layer of metal 22 to prevent sweep of the metal 22 into the thermally stable polycrystalline superabrasive table 18 beyond a desired depth. For example, copper, aluminum, silver, alloys of these, silicon, or any combination of the foregoing materials may be infiltrated into interstitial spaces between grains of the thermally stable polycrystalline table 18 to prevent sweep of the metal 22 into the polycrystalline table 18 beyond a desired depth. More specifically, nickel aluminide, nickel silicide, or a combination of these may be infiltrated into interstitial spaces between grains of the thermally stable polycrystalline table 18. Alternatively, the end of the polycrystalline superabrasive table 18 to be placed opposite the layer of metal 22 in mold 24 may be pre-infiltrated with a non-catalyst material. In other embodiments, the thermally stable polycrystalline table 18, the layer of metal 22, and the mixture of particles or a preformed substrate 20 may be subjected to hot isostatic pressing (HIP) or rapic omnidirectional compaction (ROC) to cause the layer of metal to flow and secure the polycrystalline table to the substrate 20. Consequently, the layer of metal 22 may secure the thermally stable polycrystalline table 18 to the substrate 20 while the cutting surface of the thermally stable polycrystalline table 18 may be substantially free of catalyst and metal material.
Referring to
After placement into the support structure 28, the preformed polycrystalline table 18 and the first substrate portion 20A may be subjected to a leaching process. For example, a leaching agent (e.g., aqua regia) may be introduced to the preformed polycrystalline table 18 and the first substrate portion 20A to at least substantially remove catalyst material in the interstitial spaces among interbonded grains of the material of the polycrystalline table 18 and to at least substantially remove metal matrix material from the cermet material of the first substrate portion 20A. The support structure 28 may remain at least substantially unaffected by the leaching agent. Thus, the support structure 28 may be formed from a material or materials that are resistant or impervious to conventional leaching agents, such as, for example, ceramic materials, metals, and polymers known to resist leaching agents. For example, the support structure 28 may comprise polycrystalline diamond, chrome, tungsten, polystyrene, high temperature oxides, or other materials known to resist leaching agents. Subsequent to the leaching process, the polycrystalline table 18 may be thermally stable, the polycrystalline table 18 may not be directly attached to the leached first substrate portion 20A, and the hard particles of the particle phase of the leached first substrate portion 20A may be at least substantially unbonded from one another. Accordingly, the support structure 28 may enable the thermally stable polycrystalline table 18 and the leached first substrate portion 20A to retain their shape and relative positioning during subsequent handling and processing.
The thermally stable polycrystalline table 18 and the leached first substrate portion 20A may be placed into a mold 24 (e.g., a hot press die), as shown in
Referring to
The partially leached polycrystalline table 18 and the unleached first substrate portion 20A may then be placed in an orientation in which they will remain during subsequent formation of a complete cutting element 12 (see
The thermally stable polycrystalline table 18 and the leached first substrate portion 20A may be subjected to a hot pressing process, as shown in
Referring to
The polycrystalline table 18 and the first substrate portion 20A may be at least substantially fully leached. For example, a leaching agent may at least substantially completely remove catalyst material and leach-susceptible matrix material from the polycrystalline table 18 and the first substrate portion 20A. Accordingly, when it is said that matrix material is at least substantially fully leached from the thermally stable polycrystalline table 18 and the first substrate portion 20A, it is meant that that portion of the matrix material that is susceptible to leaching is removed and matrix material that is selected to resist conventional leaching agents may remain in the first substrate portion 20A and optionally may remain in the thermally stable polycrystalline table 18. Subsequent to the leaching process, the polycrystalline table 18 may be thermally stable, the polycrystalline table 18 may optionally remain directly attached to the leached first substrate portion 20A by the leach-resistant matrix material, and the hard particles of the particle phase of the leached first substrate portion 20A may remain at least substantially bonded to one another through the leach-resistant matrix material. Thus, the leach-resistant matrix material may enable the thermally stable polycrystalline table 18 and the leached first substrate portion 20A to retain their shape and relative positioning during subsequent handling and processing in some embodiments. In embodiments where the leach-resistant matrix material does not infiltrate the polycrystalline table 18 during the conventional HTHP process, an optional support structure 28, the prior orientation of the polycrystalline table 18 and the first substrate portion 20A, or disposing the polycrystalline table 18 and the first substrate portion 20A into a mold 24 (see
The thermally stable polycrystalline table 18 and the leached first substrate portion 20A may be subjected to a hot pressing process, as shown in
While the present disclosure has been described herein with respect to certain example embodiments, those of ordinary skill in the art will recognize and appreciate that it is not so limited. Rather, many additions, deletions, and modifications to the embodiments described herein may be made without departing from the scope of embodiments of the invention as hereinafter claimed, including legal equivalents. In addition, features from one embodiment may be combined with features of another embodiment while still being encompassed within the scope of the invention as contemplated by the inventors.
Scott, Danny E., Lyons, Nicholas J.
Patent | Priority | Assignee | Title |
Patent | Priority | Assignee | Title |
4225322, | Jan 10 1978 | General Electric Company | Composite compact components fabricated with high temperature brazing filler metal and method for making same |
4954139, | Mar 31 1989 | DIAMOND INNOVATIONS, INC; GE SUPERABRASIVES, INC | Method for producing polycrystalline compact tool blanks with flat carbide support/diamond or CBN interfaces |
5244712, | Jan 15 1991 | Norton Company | Laminated diamond substrate |
5492188, | Jun 17 1994 | Baker Hughes Incorporated | Stress-reduced superhard cutting element |
20060254830, | |||
20080206576, | |||
20080302579, | |||
20090173014, | |||
WO2010083351, |
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Sep 21 2011 | SCOTT, DANNY E | Baker Hughes Incorporated | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 026967 | /0133 | |
Sep 22 2011 | LYONS, NICHOLAS J | Baker Hughes Incorporated | ASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS | 026967 | /0133 | |
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Jul 03 2017 | Baker Hughes Incorporated | BAKER HUGHES, A GE COMPANY, LLC | ENTITY CONVERSION | 047377 | /0183 |
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